公开(公告)号：US20140053566A1

公开(公告)日：2014-02-27

申请号：US13974611

申请日：2013-08-23

Applicant: ALSTOM Technology Ltd

Inventor： Adnan EROGLU ,  Ewald FREITAG

IPC: F02C7/22

CPC classification number: F23R3/34 ,  F02C7/22 ,  F02C7/228 ,  F23R3/06 ,  F23R3/20 ,  F23R3/26 ,  F23R3/346 ,  F23R3/42 ,  F23R2900/00014 ,  F23R2900/03042 ,  F23R2900/03341 ,  Y02E20/14

Abstract: The invention relates a method for mixing a dilution air with a hot main flow in a sequential combustion system of a gas turbine, wherein the gas turbine essentially comprises at least one compressor, a first combustor which is connected downstream to the compressor The hot gases of the first combustor are admitted to at least one intermediate turbine or directly or indirectly to at least one second combustor, wherein the hot gases of the second combustor are admitted to a further turbine or directly or indirectly to an energy recovery. The method comprising a coaxial injection of first combustor liner cooling air with second combustor liner cooling air having a sufficient excess pressure margin with respect to the second combustor liner cooling air

Abstract translation: 本发明涉及一种用于在燃气轮机的顺序燃烧系统中混合稀释空气与热主流的方法，其中燃气轮机基本上包括至少一个压缩机，第一燃烧器，其连接在压缩机的下游。 第一燃烧器被允许进入至少一个中间涡轮机，或者直接或间接地接纳到至少一个第二燃烧器，其中第二燃烧器的热气体被允许进一步涡轮机，或直接或间接地进入能量回收。 该方法包括：第一燃烧器衬套冷却空气同轴喷射，第二燃烧器衬套冷却空气相对于第二燃烧器衬套冷却空气具有足够的超压余量